Return-Path: Received: from smtp4.gateway.net ([208.230.117.248]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Tue, 14 Mar 2000 10:54:53 -0500 Received: from oemcomputer (1Cust59.tnt10.chi5.da.uu.net [63.22.154.59]) by smtp4.gateway.net (8.9.3/8.9.3) with SMTP id LAA23487 for ; Tue, 14 Mar 2000 11:00:30 -0500 (EST) Message-ID: <004201bf8dce$d9864ce0$289a163f@oemcomputer> From: "bobjude" To: "Lancair Mail List" Subject: LNC2 Oil Cooler Venting Date: Tue, 14 Mar 2000 09:51:50 -0600 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Dan Olsen, This is what I did to provide air to the oil cooler on my L320. Take the NACA duct layout from page 416, Figure 353 and scale it up to 2 times the size shown. Cut this opening in the lower left side of the bottom cowling. Position the NACA duct and the oil cooler on the firewall so that a short fiberglass duct can be constructed between the two with slip joint for cowl removal. This is the air inlet for the oil cooler. The exit air from the oil cooler is directed downward toward the top of the exhaust pipes by a fiberglass shroud that is attached to the oil cooler. I believe this helps to keep hot air away from fuel lines, gascolator etc.. I have heard of more builders who have had problems with CHT in flight, so I would be leery about taking any of the cooling air from the top plenum. My oil cooler arrangement has worked well for me, even on very hot (100F) days. Be sure to get a 9 vane cooler. Bob Jude N65BJ >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>